[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 15th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 905 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 660)
---------------------------------------
Vector Time (GMT): 2015/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2217428
58 A = 6776749
22 meter
Y = -3599555
15 meter E =
0008599
Z = 5291167
52 I = 51
44904
XDOT = 6703
964792 Wp = 45
81367
YDOT = 3724
566316 meter/sec RA = 207
45056 deg
ZDOT = -269
547981 TA = 46
79649
MA = 46
72469
Ha = 222
556 n
mi
Hp = 212
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7275028
14 X = 2231811
78
Y = -11809564
15 feet Y = -3574677
39 meter
Z = 17359473
50 Z = 5301974
95
XDOT = 21994
635144 XDOT = 6663
126920
YDOT = 12219
705761 feet/sec YDOT = 3799
306103 meter/sec
ZDOT = -884
343770 ZDOT = -237
080300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2248771
10 X = -685425
43
Y = 13626978
75 feet Y = 4153503
12 meter
Z = 17406655
01 Z = 5305548
45
XDOT = -23974
943530 XDOT = -7307
562788
YDOT = -2979
173353 feet/sec YDOT = -908
052038 meter/sec
ZDOT = -744
920837 ZDOT = -227
051871
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15287
54786807
00016717 00000-0 10270-3 0 9005
2 25544 51
6431 208
3125 0006685 33
6348 326
5228 15
54338035 6613
Satellite: ISS
Catalog Number: 25544
Epoch time: 15287
54786807 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 208
3125 deg
Eccentricity:
0006685
Arg of perigee: 33
6348 deg
Mean anomaly: 326
5228 deg
Mean motion: 15
54338035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 661
Checksum: 312
Coasting Arc #2 (Orbit 675)
---------------------------------------
Vector Time (GMT): 2015/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3818910
75 A = 6778367
14 meter
Y = 2672353
52 meter E =
0016191
Z = -4934764
42 I = 51
48335
XDOT = -5899
960646 Wp = 83
52383
YDOT = -4347
562057 meter/sec RA = 202
43748 deg
ZDOT = 2219
557954 TA = 208
17599
MA = 208
26369
Ha = 222
741 n
mi
Hp = 212
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12529234
75 X = -3824538
02
Y = 8767564
05 feet Y = 2629616
00 meter
Z = -16190171
99 Z = -4953330
31
XDOT = -19356
826266 XDOT = -5861
688684
YDOT = -14263
655044 feet/sec YDOT = -4413
325102 meter/sec
ZDOT = 7282
014285 ZDOT = 2190
989799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8044067
76 X = 2451831
85
Y = -12904719
64 feet Y = -3933358
55 meter
Z = -16270671
67 Z = -4959300
73
XDOT = 22478
894966 XDOT = 6851
567186
YDOT = 5018
342961 feet/sec YDOT = 1529
590935 meter/sec
ZDOT = 7159
495323 ZDOT = 2182
214174
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15288
51228543
00016717 00000-0 10270-3 0 9012
2 25544 51
6434 203
5031 0006777 37
7233 322
4394 15
54320481 6760
Satellite: ISS
Catalog Number: 25544
Epoch time: 15288
51228543 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 203
5031 deg
Eccentricity:
0006777
Arg of perigee: 37
7233 deg
Mean anomaly: 322
4394 deg
Mean motion: 15
54320481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 676
Checksum: 296
Coasting Arc #3 (Orbit 691)
---------------------------------------
Vector Time (GMT): 2015/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5214967
92 A = 6781873
13 meter
Y = -1683942
78 meter E =
0016739
Z = 3987541
59 I = 51
52452
XDOT = 4566
341539 Wp = 64
84288
YDOT = 4728
582606 meter/sec RA = 197
43427 deg
ZDOT = -3955
053942 TA = 66
43270
MA = 66
25697
Ha = 222
724 n
mi
Hp = 212
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17109474
81 X = 5214040
15
Y = -5524746
66 feet Y = -1625630
44 meter
Z = 13082485
54 Z = 4012873
37
XDOT = 14981
435495 XDOT = 4532
338614
YDOT = 15513
722462 feet/sec YDOT = 4779
456007 meter/sec
ZDOT = -12975
898761 ZDOT = -3932
954000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13339112
75 X = -4065761
57
Y = 11935118
24 feet Y = 3637824
04 meter
Z = 13192020
52 Z = 4020927
85
XDOT = -19179
178476 XDOT = -5845
813599
YDOT = -7125
559067 feet/sec YDOT = -2171
870404 meter/sec
ZDOT = -12881
327370 ZDOT = -3926
228582
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15289
54098521
00016717 00000-0 10270-3 0 9028
2 25544 51
6429 198
3735 0006782 41
8339 318
3331 15
54333279 6927
Satellite: ISS
Catalog Number: 25544
Epoch time: 15289
54098521 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 198
3735 deg
Eccentricity:
0006782
Arg of perigee: 41
8339 deg
Mean anomaly: 318
3331 deg
Mean motion: 15
54333279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 692
Checksum: 329
Coasting Arc #4 (Orbit 706)
---------------------------------------
Vector Time (GMT): 2015/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6206803
82 A = 6785611
56 meter
Y = 766721
87 meter E =
0011650
Z = -2629080
56 I = 51
56845
XDOT = -2803
048402 Wp = 49
56970
YDOT = -4861
990047 meter/sec RA = 192
44359 deg
ZDOT = 5222
237697 TA = 280
77946
MA = 280
91058
Ha = 222
725 n
mi
Hp = 212
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20363529
61 X = -6202144
82
Y = 2515491
70 feet Y = 697339
17 meter
Z = -8625592
39 Z = -2659221
40
XDOT = -9196
353025 XDOT = -2773
840345
YDOT = -15951
410915 feet/sec YDOT = -4893
171920 meter/sec
ZDOT = 17133
325778 ZDOT = 5208
692007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17374398
37 X = 5295716
62
Y = -10810604
58 feet Y = -3295072
28 meter
Z = -8755740
42 Z = -2668749
68
XDOT = 14355
147992 XDOT = 4375
449108
YDOT = 9300
355919 feet/sec YDOT = 2834
748484 meter/sec
ZDOT = 17075
667082 ZDOT = 5204
663327
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15290
50537998
00016717 00000-0 10270-3 0 9033
2 25544 51
6434 193
5640 0006747 44
9250 315
2448 15
54366310 7076
Satellite: ISS
Catalog Number: 25544
Epoch time: 15290
50537998 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 193
5640 deg
Eccentricity:
0006747
Arg of perigee: 44
9250 deg
Mean anomaly: 315
2448 deg
Mean motion: 15
54366310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 707
Checksum: 313
Coasting Arc #5 (Orbit 722)
---------------------------------------
Vector Time (GMT): 2015/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6720571
74 A = 6788299
40 meter
Y = 150127
00 meter E =
0016503
Z = 914078
61 I = 51
60825
XDOT = 709
122119 Wp = 101
96837
YDOT = 4822
669918 meter/sec RA = 187
46491 deg
ZDOT = -5918
638496 TA = 68
13289
MA = 67
95747
Ha = 222
850 n
mi
Hp = 212
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22049119
87 X = 6713953
15
Y = 492542
64 feet Y = 225243
91 meter
Z = 2998945
58 Z = 946710
39
XDOT = 2326
516140 XDOT = 683
892231
YDOT = 15822
407866 feet/sec YDOT = 4830
458377 meter/sec
ZDOT = -19418
105301 ZDOT = -5915
255213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20045328
36 X = -6109816
08
Y = 9150244
99 feet Y = 2788994
67 meter
Z = 3139711
39 Z = 956984
03
XDOT = -8428
606970 XDOT = -2569
039404
YDOT = -11712
621527 feet/sec YDOT = -3570
007041 meter/sec
ZDOT = -19404
278814 ZDOT = -5914
424183
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15291
53405770
00016717 00000-0 10270-3 0 9040
2 25544 51
6432 188
4336 0006697 49
1400 311
0332 15
54349498 7239
Satellite: ISS
Catalog Number: 25544
Epoch time: 15291
53405770 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 188
4336 deg
Eccentricity:
0006697
Arg of perigee: 49
1400 deg
Mean anomaly: 311
0332 deg
Mean motion: 15
54349498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 723
Checksum: 303
Coasting Arc #6 (Orbit 738)
---------------------------------------
Vector Time (GMT): 2015/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6654131
58 A = 6788320
31 meter
Y = -967970
39 meter E =
0020131
Z = 856332
14 I = 51
64033
XDOT = 1450
052800 Wp = 53
26823
YDOT = -4640
459910 meter/sec RA = 182
49195 deg
ZDOT = 5937
392164 TA = 316
00308
MA = 316
16315
Ha = 222
852 n
mi
Hp = 212
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21831140
37 X = -6646972
76
Y = -3175755
88 feet Y = -1042341
21 meter
Z = 2809488
64 Z = 824024
58
XDOT = 4757
391075 XDOT = 1472
993685
YDOT = -15224
606004 feet/sec YDOT = -4624
115868 meter/sec
ZDOT = 19479
633083 ZDOT = 5944
492329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20933214
14 X = 6380443
67
Y = -7017673
46 feet Y = -2138986
87 meter
Z = 2670233
44 Z = 813887
15
XDOT = 2217
467784 XDOT = 675
884181
YDOT = 14149
920055 feet/sec YDOT = 4312
895633 meter/sec
ZDOT = 19511
012583 ZDOT = 5946
956635
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15292
56272311
00016717 00000-0 10270-3 0 9058
2 25544 51
6433 183
3033 0006772 51
1671 309
0085 15
54381518 7393
Satellite: ISS
Catalog Number: 25544
Epoch time: 15292
56272311 = yrday
fracday
Element set: 905
Inclination: 51
6433 deg
RA of node: 183
3033 deg
Eccentricity:
0006772
Arg of perigee: 51
1671 deg
Mean anomaly: 309
0085 deg
Mean motion: 15
54381518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 739
Checksum: 295
Coasting Arc #7 (Orbit 753)
---------------------------------------
Vector Time (GMT): 2015/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6016307
92 A = 6785831
55 meter
Y = 1787988
11 meter E =
0009398
Z = -2588443
64 I = 51
66414
XDOT = -3534
676954 Wp = 87
41083
YDOT = 4311
458381 meter/sec RA = 177
51789 deg
ZDOT = -5253
537358 TA = 121
67116
MA = 121
57948
Ha = 222
836 n
mi
Hp = 212
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19738543
04 X = 6008440
91
Y = 5866102
72 feet Y = 1855222
29 meter
Z = -8492269
16 Z = -2559236
41
XDOT = -11596
709167 XDOT = -3557
105966
YDOT = 14145
204663 feet/sec YDOT = 4271
805576 meter/sec
ZDOT = -17236
014953 ZDOT = -5270
763093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20244316
83 X = -6170467
77
Y = 4038451
45 feet Y = 1230920
00 meter
Z = -8366506
06 Z = -2550111
05
XDOT = 3862
293892 XDOT = 1177
227178
YDOT = -16391
307044 feet/sec YDOT = -4996
070387 meter/sec
ZDOT = -17311
044364 ZDOT = -5276
406322
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15293
52708671
00016717 00000-0 10270-3 0 9069
2 25544 51
6436 178
4936 0006560 54
7997 305
3769 15
54381950 7543
Satellite: ISS
Catalog Number: 25544
Epoch time: 15293
52708671 = yrday
fracday
Element set: 906
Inclination: 51
6436 deg
RA of node: 178
4936 deg
Eccentricity:
0006560
Arg of perigee: 54
7997 deg
Mean anomaly: 305
3769 deg
Mean motion: 15
54381950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 754
Checksum: 346
Coasting Arc #8 (Orbit 769)
---------------------------------------
Vector Time (GMT): 2015/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4859754
84 A = 6781893
76 meter
Y = -2534306
47 meter E =
0016683
Z = 3978738
17 I = 51
68300
XDOT = 5294
832926 Wp = 84
71288
YDOT = -3872
103162 meter/sec RA = 172
53594 deg
ZDOT = 3988
021871 TA = 323
76913
MA = 323
88201
Ha = 222
993 n
mi
Hp = 212
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15944077
55 X = -4850381
86
Y = -8314653
78 feet Y = -2588598
77 meter
Z = 13053602
93 Z = 3955153
10
XDOT = 17371
499101 XDOT = 5318
365659
YDOT = -12703
750530 feet/sec YDOT = -3812
760991 meter/sec
ZDOT = 13084
061257 ZDOT = 4013
800866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18049955
28 X = 5501626
37
Y = -427808
41 feet Y = -130396
00 meter
Z = 12952209
08 Z = 3947833
33
XDOT = -9069
695797 XDOT = -2764
443279
YDOT = 18139
351931 feet/sec YDOT = 5528
874469 meter/sec
ZDOT = 13195
947400 ZDOT = 4022
124768
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15294
55573137
00016717 00000-0 10270-3 0 9071
2 25544 51
6436 173
3631 0006788 58
0036 302
1776 15
54407454 7701
Satellite: ISS
Catalog Number: 25544
Epoch time: 15294
55573137 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 173
3631 deg
Eccentricity:
0006788
Arg of perigee: 58
0036 deg
Mean anomaly: 302
1776 deg
Mean motion: 15
54407454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 770
Checksum: 316
Coasting Arc #9 (Orbit 784)
---------------------------------------
Vector Time (GMT): 2015/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3300411
10 A = 6778127
33 meter
Y = 3274171
14 meter E =
0018708
Z = -4949963
26 I = 51
70217
XDOT = -6562
648894 Wp = 69
26819
YDOT = 3250
006663 meter/sec RA = 167
54462 deg
ZDOT = -2226
298381 TA = 178
98018
MA = 178
97636
Ha = 222
786 n
mi
Hp = 212
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10828120
39 X = 3287598
56
Y = 10742031
30 feet Y = 3311006
45 meter
Z = -16240036
95 Z = -4933961
73
XDOT = -21531
000309 XDOT = -6587
688861
YDOT = 10662
751520 feet/sec YDOT = 3176
478599 meter/sec
ZDOT = -7304
128545 ZDOT = -2258
239908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14821170
62 X = -4517492
80
Y = -3897973
49 feet Y = -1188102
32 meter
Z = -16171485
15 Z = -4929068
67
XDOT = 13073
985836 XDOT = 3984
950883
YDOT = -18838
936006 feet/sec YDOT = -5742
107694 meter/sec
ZDOT = -7442
530168 ZDOT = -2268
483195
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15295
52007409
00016717 00000-0 10270-3 0 9084
2 25544 51
6435 168
5532 0006625 60
2946 299
8866 15
54450789 7858
Satellite: ISS
Catalog Number: 25544
Epoch time: 15295
52007409 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 168
5532 deg
Eccentricity:
0006625
Arg of perigee: 60
2946 deg
Mean anomaly: 299
8866 deg
Mean motion: 15
54450789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 785
Checksum: 346
Coasting Arc #10 (Orbit 800)
---------------------------------------
Vector Time (GMT): 2015/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1486649
45 A = 6776394
58 meter
Y = -3925923
74 meter E =
0008739
Z = 5312095
88 I = 51
72775
XDOT = 7267
049304 Wp = 74
91046
YDOT = -2462
871168 meter/sec RA = 162
54768 deg
ZDOT = 215
500367 TA = 13
05150
MA = 13
02890
Ha = 222
854 n
mi
Hp = 211
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4877458
81 X = -1468442
82
Y = -12880327
24 feet Y = -3942446
11 meter
Z = 17428136
07 Z = 5304918
55
XDOT = 23842
025274 XDOT = 7293
002789
YDOT = -8080
285983 feet/sec YDOT = -2381
461092 meter/sec
ZDOT = 707
022201 ZDOT = 250
866016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10871459
45 X = 3313620
84
Y = 8518279
04 feet Y = 2596371
45 meter
Z = 17397777
24 Z = 5302842
50
XDOT = -15734
752211 XDOT = -4795
952474
YDOT = 18337
775264 feet/sec YDOT = 5589
353900 meter/sec
ZDOT = 860
095198 ZDOT = 262
157016
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15296
54869735
00016717 00000-0 10270-3 0 9096
2 25544 51
6437 163
4229 0006626 64
5483 295
6355 15
54460681 8019
Satellite: ISS
Catalog Number: 25544
Epoch time: 15296
54869735 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 163
4229 deg
Eccentricity:
0006626
Arg of perigee: 64
5483 deg
Mean anomaly: 295
6355 deg
Mean motion: 15
54460681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 801
Checksum: 339
Coasting Arc #11 (Orbit 815)
---------------------------------------
Vector Time (GMT): 2015/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -371077
87 A = 6777373
03 meter
Y = 4486859
50 meter E =
0018928
Z = -5082394
09 I = 51
76042
XDOT = -7290
400100 Wp = 91
96377
YDOT = 1457
074924 meter/sec RA = 157
55083 deg
ZDOT = 1823
866741 TA = 195
66561
MA = 195
72425
Ha = 222
764 n
mi
Hp = 211
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1217447
07 X = -396534
68
Y = 14720667
66 feet Y = 4482566
97 meter
Z = -16674521
29 Z = -5084259
07
XDOT = -23918
635500 XDOT = -7315
011430
YDOT = 4780
429541 feet/sec YDOT = 1375
411451 meter/sec
ZDOT = 5983
814767 ZDOT = 1788
390889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6796425
40 X = -2071550
46
Y = -13103292
12 feet Y = -3993883
44 meter
Z = -16683291
98 Z = -5085067
40
XDOT = 16905
616144 XDOT = 5152
831801
YDOT = -16170
117256 feet/sec YDOT = -4928
651740 meter/sec
ZDOT = 5830
412289 ZDOT = 1777
109666
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15297
51302145
00016717 00000-0 10270-3 0 9103
2 25544 51
6427 158
6122 0006555 67
1674 293
0171 15
54481853 8166
Satellite: ISS
Catalog Number: 25544
Epoch time: 15297
51302145 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 158
6122 deg
Eccentricity:
0006555
Arg of perigee: 67
1674 deg
Mean anomaly: 293
0171 deg
Mean motion: 15
54481853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 816
Checksum: 303
Coasting Arc #12 (Orbit 831)
---------------------------------------
Vector Time (GMT): 2015/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2144202
55 A = 6780567
97 meter
Y = -4850288
12 meter E =
0016536
Z = 4214948
31 I = 51
80072
XDOT = 6731
888831 Wp = 72
68353
YDOT = -234
316882 meter/sec RA = 152
56333 deg
ZDOT = -3677
557097 TA = 54
96650
MA = 54
81145
Ha = 222
644 n
mi
Hp = 211
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7034785
28 X = 2177805
24
Y = -15913018
77 feet Y = -4826121
88 meter
Z = 13828570
58 Z = 4225446
80
XDOT = 22086
249447 XDOT = 6751
873248
YDOT = -768
756175 feet/sec YDOT = -158
925127 meter/sec
ZDOT = -12065
476039 ZDOT = -3644
805658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2755746
57 X = 839951
56
Y = 17141784
07 feet Y = 5224815
78 meter
Z = 13874683
22 Z = 4229003
44
XDOT = -16980
792919 XDOT = -5175
745682
YDOT = 12425
412461 feet/sec YDOT = 3787
265718 meter/sec
ZDOT = -11924
020600 ZDOT = -3634
441479
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15298
54162242
00016717 00000-0 10270-3 0 9110
2 25544 51
6427 153
4817 0006480 69
6918 290
4930 15
54528356 8327
Satellite: ISS
Catalog Number: 25544
Epoch time: 15298
54162242 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 153
4817 deg
Eccentricity:
0006480
Arg of perigee: 69
6918 deg
Mean anomaly: 290
4930 deg
Mean motion: 15
54528356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 832
Checksum: 321
Coasting Arc #13 (Orbit 846)
---------------------------------------
Vector Time (GMT): 2015/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3602093
71 A = 6784650
45 meter
Y = 4974347
74 meter E =
0011011
Z = -2887157
54 I = 51
84026
XDOT = -5630
080358 Wp = 70
65655
YDOT = -1145
080751 meter/sec RA = 147
58798 deg
ZDOT = 5070
648276 TA = 256
58731
MA = 256
71006
Ha = 222
714 n
mi
Hp = 211
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11817892
74 X = -3643425
28
Y = 16320038
53 feet Y = 4933835
37 meter
Z = -9472301
64 Z = -2904757
13
XDOT = -18471
392250 XDOT = -5641
489262
YDOT = -3756
826611 feet/sec YDOT = -1208
103312 meter/sec
ZDOT = 16635
985156 ZDOT = 5043
270168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 726044
65 X = 221298
41
Y = -20100201
91 feet Y = -6126541
54 meter
Z = -9549109
24 Z = -2910568
50
XDOT = 16073
113390 XDOT = 4899
084961
YDOT = -7236
851567 feet/sec YDOT = -2205
792358 meter/sec
ZDOT = 16517
945676 ZDOT = 5034
669842
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15299
50592815
00016717 00000-0 10270-3 0 9121
2 25544 51
6410 148
6709 0006452 73
9748 286
2115 15
54500651 8475
Satellite: ISS
Catalog Number: 25544
Epoch time: 15299
50592815 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 148
6709 deg
Eccentricity:
0006452
Arg of perigee: 73
9748 deg
Mean anomaly: 286
2115 deg
Mean motion: 15
54500651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 847
Checksum: 320
Coasting Arc #14 (Orbit 862)
---------------------------------------
Vector Time (GMT): 2015/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4710253
77 A = 6787552
11 meter
Y = -4739159
17 meter E =
0018883
Z = 1155714
59 I = 51
87640
XDOT = 4135
573666 Wp = 108
20192
YDOT = 2656
451025 meter/sec RA = 142
62598 deg
ZDOT = -5888
907937 TA = 59
28572
MA = 59
09982
Ha = 222
718 n
mi
Hp = 211
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15453588
49 X = 4757283
94
Y = -15548422
48 feet Y = -4686222
95 meter
Z = 3791714
55 Z = 1178711
33
XDOT = 13568
155072 XDOT = 4134
168112
YDOT = 8715
390502 feet/sec YDOT = 2702
689418 meter/sec
ZDOT = -19320
564097 ZDOT = -5868
821194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3838322
20 X = -1169920
61
Y = 21565367
03 feet Y = 6573123
87 meter
Z = 3891807
50 Z = 1186222
93
XDOT = -14644
321039 XDOT = -4463
589053
YDOT = 906
751886 feet/sec YDOT = 276
377975 meter/sec
ZDOT = -19234
253579 ZDOT = -5862
600491
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15300
53450898
00016717 00000-0 10270-3 0 9132
2 25544 51
6408 143
5398 0006520 76
9483 283
2398 15
54535919 8638
Satellite: ISS
Catalog Number: 25544
Epoch time: 15300
53450898 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 143
5398 deg
Eccentricity:
0006520
Arg of perigee: 76
9483 deg
Mean anomaly: 283
2398 deg
Mean motion: 15
54535919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 863
Checksum: 334
Coasting Arc #15 (Orbit 878)
---------------------------------------
Vector Time (GMT): 2015/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5323133
57 A = 6787996
48 meter
Y = 4147546
18 meter E =
0019014
Z = 661299
09 I = 51
90101
XDOT = -2450
796471 Wp = 61
71014
YDOT = -4119
824901 meter/sec RA = 137
66914 deg
ZDOT = 5989
311076 TA = 305
40907
MA = 305
58651
Ha = 222
721 n
mi
Hp = 211
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17464348
98 X = -5372329
24
Y = 13607434
97 feet Y = 4087744
35 meter
Z = 2169616
45 Z = 635319
91
XDOT = -8040
670838 XDOT = -2433
640076
YDOT = -13516
485895 feet/sec YDOT = -4147
135076 meter/sec
ZDOT = 19649
970721 ZDOT = 5977
447144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6262764
13 X = 1908890
51
Y = -21246663
08 feet Y = -6475982
91 meter
Z = 2056720
87 Z = 626888
52
XDOT = 12965
703243 XDOT = 3951
946349
YDOT = 5759
887539 feet/sec YDOT = 1755
613722 meter/sec
ZDOT = 19599
415647 ZDOT = 5973
901889
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15301
56307944
00016717 00000-0 10270-3 0 9140
2 25544 51
6393 138
4075 0006449 81
5339 278
6545 15
54531380 8795
Satellite: ISS
Catalog Number: 25544
Epoch time: 15301
56307944 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 138
4075 deg
Eccentricity:
0006449
Arg of perigee: 81
5339 deg
Mean anomaly: 278
6545 deg
Mean motion: 15
54531380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 879
Checksum: 329
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